FREE VIBRATION ANALYSIS OF AN AIRCRAFT WING BY CONSIDERING AS A CANTILEVER BEAM
Yıl: 2019 Cilt: 7 Sayı: 1 Sayfa Aralığı: 12 - 21 Metin Dili: İngilizce DOI: 10.15317/Scitech.2019.178 İndeks Tarihi: 21-06-2020
FREE VIBRATION ANALYSIS OF AN AIRCRAFT WING BY CONSIDERING AS A CANTILEVER BEAM
Öz: The present paper presents the modal analyses of a NACA 4415 airfoil profiled wing.Theoretical and numerical calculations are performed by considering the aircraft wing as a cantileverbeam. The model is created and modal analyses are performed by using commercially availablepackages of SolidWorks and Ansys, respectively. The natural frequencies and the related mode shapesare obtained. The results of theoretical calculations are compared with the numerical modal analyses.The study has a conclusion that an aircraft wing can be considered as a cantilever beam that by ignoringthe whole forces on the aircraft (except for gravity).
Anahtar Kelime: Ankastre Kiriş Olarak Düşünülen Bir Uçak Kanadının Serbest Titreşim Analizi
Öz: Bu çalışmada NACA 4415 profiline sahip uçak kanadının modal analizi sunulmuştur. Uçak kanadı bir ankastre kiriş olarak düşünülerek teorik ve nümerik hesaplamalar gerçekleştirilmiştir. Kanadın modellenmesi ve modal analizi ticari paket programları SolidWorks ve Ansys ile yapılmıştır. Analiz sonucunda uçak kanadı modelinin doğal frekansı ve buna bağlı mod şekilleri elde edilmiştir. Teorik hesaplar neticesinde elde edilen sonuçlar nümerik modal analiz sonuçları ile karşılaştırılmıştır. Çalışmadan elde edilen sonuç, eğer yer çekimi kuvveti hariç diğer tüm kuvvetler ihmal edilirse, uçak kanadının ankastre bir kiriş olarak değerlendirilebileceği yönündedir.
Anahtar Kelime: Belge Türü: Makale Makale Türü: Araştırma Makalesi Erişim Türü: Erişime Açık
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| APA | DEMİRTAŞ A, Bayraktar M (2019). FREE VIBRATION ANALYSIS OF AN AIRCRAFT WING BY CONSIDERING AS A CANTILEVER BEAM. , 12 - 21. 10.15317/Scitech.2019.178 |
| Chicago | DEMİRTAŞ Ali,Bayraktar Meral FREE VIBRATION ANALYSIS OF AN AIRCRAFT WING BY CONSIDERING AS A CANTILEVER BEAM. (2019): 12 - 21. 10.15317/Scitech.2019.178 |
| MLA | DEMİRTAŞ Ali,Bayraktar Meral FREE VIBRATION ANALYSIS OF AN AIRCRAFT WING BY CONSIDERING AS A CANTILEVER BEAM. , 2019, ss.12 - 21. 10.15317/Scitech.2019.178 |
| AMA | DEMİRTAŞ A,Bayraktar M FREE VIBRATION ANALYSIS OF AN AIRCRAFT WING BY CONSIDERING AS A CANTILEVER BEAM. . 2019; 12 - 21. 10.15317/Scitech.2019.178 |
| Vancouver | DEMİRTAŞ A,Bayraktar M FREE VIBRATION ANALYSIS OF AN AIRCRAFT WING BY CONSIDERING AS A CANTILEVER BEAM. . 2019; 12 - 21. 10.15317/Scitech.2019.178 |
| IEEE | DEMİRTAŞ A,Bayraktar M "FREE VIBRATION ANALYSIS OF AN AIRCRAFT WING BY CONSIDERING AS A CANTILEVER BEAM." , ss.12 - 21, 2019. 10.15317/Scitech.2019.178 |
| ISNAD | DEMİRTAŞ, Ali - Bayraktar, Meral. "FREE VIBRATION ANALYSIS OF AN AIRCRAFT WING BY CONSIDERING AS A CANTILEVER BEAM". (2019), 12-21. https://doi.org/10.15317/Scitech.2019.178 |
| APA | DEMİRTAŞ A, Bayraktar M (2019). FREE VIBRATION ANALYSIS OF AN AIRCRAFT WING BY CONSIDERING AS A CANTILEVER BEAM. Selçuk Üniversitesi Mühendislik Bilim ve Teknoloji Dergisi, 7(1), 12 - 21. 10.15317/Scitech.2019.178 |
| Chicago | DEMİRTAŞ Ali,Bayraktar Meral FREE VIBRATION ANALYSIS OF AN AIRCRAFT WING BY CONSIDERING AS A CANTILEVER BEAM. Selçuk Üniversitesi Mühendislik Bilim ve Teknoloji Dergisi 7, no.1 (2019): 12 - 21. 10.15317/Scitech.2019.178 |
| MLA | DEMİRTAŞ Ali,Bayraktar Meral FREE VIBRATION ANALYSIS OF AN AIRCRAFT WING BY CONSIDERING AS A CANTILEVER BEAM. Selçuk Üniversitesi Mühendislik Bilim ve Teknoloji Dergisi, vol.7, no.1, 2019, ss.12 - 21. 10.15317/Scitech.2019.178 |
| AMA | DEMİRTAŞ A,Bayraktar M FREE VIBRATION ANALYSIS OF AN AIRCRAFT WING BY CONSIDERING AS A CANTILEVER BEAM. Selçuk Üniversitesi Mühendislik Bilim ve Teknoloji Dergisi. 2019; 7(1): 12 - 21. 10.15317/Scitech.2019.178 |
| Vancouver | DEMİRTAŞ A,Bayraktar M FREE VIBRATION ANALYSIS OF AN AIRCRAFT WING BY CONSIDERING AS A CANTILEVER BEAM. Selçuk Üniversitesi Mühendislik Bilim ve Teknoloji Dergisi. 2019; 7(1): 12 - 21. 10.15317/Scitech.2019.178 |
| IEEE | DEMİRTAŞ A,Bayraktar M "FREE VIBRATION ANALYSIS OF AN AIRCRAFT WING BY CONSIDERING AS A CANTILEVER BEAM." Selçuk Üniversitesi Mühendislik Bilim ve Teknoloji Dergisi, 7, ss.12 - 21, 2019. 10.15317/Scitech.2019.178 |
| ISNAD | DEMİRTAŞ, Ali - Bayraktar, Meral. "FREE VIBRATION ANALYSIS OF AN AIRCRAFT WING BY CONSIDERING AS A CANTILEVER BEAM". Selçuk Üniversitesi Mühendislik Bilim ve Teknoloji Dergisi 7/1 (2019), 12-21. https://doi.org/10.15317/Scitech.2019.178 |
